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Tangential-Slot Film Cooling on a Plate in Supersonic Flow. Comparison of Calculation and Experiment

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Abstract

The boundary layer flow on a plate in the presence of tangential-slot supersonic gas injection into the supersonic flow is studied numerically. The dependence of the film-cooling effectiveness on the slot film parameters, i.e. gas temperature, mass flow, slot height, and the gas-film and free-stream Mach numbers, is determined. The calculation results are compared with experimental data.

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REFERENCES

  1. V. G. Lushchik and A. E. Yakubenko, “Tangential-slot film cooling on a plate. Comparison of calculation and experiment,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 6, 48 (1997).

  2. V. G. Lushchik and A. E. Yakubenko, “Comparative analysis of turbulence models for calculating the boundary layer,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 1, 44 (1998).

  3. V. G. Lushchik and A. E. Yakubenko, “Supersonic boundary layer on a plate. Comparison of calculation and experiment,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 6, 64 (1998).

  4. V. G. Lushchik, A. A. Pavel'ev, A. I. Reshmin, and A. E. Yakubenko, “The effect of boundary conditions on the transition to turbulence in the boundary layer on a plate for high-level external disturbances,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 6, 11 (1999).

  5. V. G. Lushchik and A. E. Yakubenko, “Tangential-slot film cooling in a nozzle. Comparison of calculation and experiment,” Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 6, 34 (2000).

  6. G. N. Abramovich, V. B. Kuz'mich, A. N. Sekundov, and I. P. Smirnova, “Experimental and numerical study of a supersonic wall jet in co-current supersonic flow,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 25 (1972).

  7. A. M. Cary, Jr. and J. N. Hefner, “Film-cooling effectiveness and skin friction in hypersonic turbulent flow,” AIAA J., 10, No. 9, 1188 (1972).

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  8. W. K. Burns and J. L. Stollery, “The influence of foreign gas injection and slot geometry on film cooling effectiveness,” Intern. J. Heat Mass Transfer, 12, No. 8, 935 (1969).

    Google Scholar 

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Authors
  1. V. G. Lushchik
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  2. A. E. Yakubenko
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Lushchik, V.G., Yakubenko, A.E. Tangential-Slot Film Cooling on a Plate in Supersonic Flow. Comparison of Calculation and Experiment. Fluid Dynamics 36, 926–933 (2001). https://doi.org/10.1023/A:1017914710250

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  • DOI: https://doi.org/10.1023/A:1017914710250

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